Flutter prediction methods for aeroelastic design optimization

Journal of Aircraft

Volumn 38, Issue 3, 2001, Pages 557-559

  Pidaparti, R M V ^a   Tischler, V A ^b   Venkayya, V B ^b  

^a Indiana University Purdue University Indianapolis   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DAMPING; DESIGN; EIGENVALUES AND EIGENFUNCTIONS; OPTIMIZATION; STIFFNESS MATRIX; WINGS;

AIRCRAFT DESIGN; EIGENVECTOR ORIENTATIONS; FLUTTER PREDICTION METHODS;

FLUTTER (AERODYNAMICS);

EID: 0035333094     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2797     Document Type: Article

References (5)

1. Automated structural optimization system (ASTROS)
2. Flutter prediction using eigenvector orientation approach
3. Flutter instability tracking for aeroelastic design optimization studies
4. Unsteady aeroelastic analysis capabilities in NASTRAN